Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:basedOn |
gptkb:Mil_Mi-6
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:crew |
5
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
1957
|
| gptkbp:height |
9.86 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mi-6A
|
| gptkbp:introduced |
1962
|
| gptkbp:length |
33.18 m
|
| gptkbp:mainRotorDiameter |
35 m
|
| gptkbp:manufacturer |
gptkb:Mil_Moscow_Helicopter_Plant
|
| gptkbp:maximumSpeed |
300 km/h
|
| gptkbp:maxTakeoffWeight |
42,500 kg
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:primaryUser |
gptkb:Soviet_Air_Force
|
| gptkbp:range |
620 km
|
| gptkbp:role |
heavy transport helicopter
|
| gptkbp:status |
retired
|
| gptkbp:bfsParent |
gptkb:Mil_Mi-6
gptkb:Mi-6 |
| gptkbp:bfsLayer |
6
|